CN206259837U - Horizontal stage electric machine, head and aircraft - Google Patents
Horizontal stage electric machine, head and aircraft Download PDFInfo
- Publication number
- CN206259837U CN206259837U CN201621230631.3U CN201621230631U CN206259837U CN 206259837 U CN206259837 U CN 206259837U CN 201621230631 U CN201621230631 U CN 201621230631U CN 206259837 U CN206259837 U CN 206259837U
- Authority
- CN
- China
- Prior art keywords
- threading hole
- electric machine
- stage electric
- horizontal stage
- head
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000004804 winding Methods 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K21/00—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets
- H02K21/12—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets with stationary armatures and rotating magnets
- H02K21/24—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets with stationary armatures and rotating magnets with magnets axially facing the armatures, e.g. hub-type cycle dynamos
Abstract
The utility model discloses a kind of horizontal stage electric machine, head and aircraft, the horizontal stage electric machine includes rotor, stator and magnet ring, the first threading hole is provided with the centre position of the stator, the position of correspondence first threading hole is provided with the second threading hole on the rotor, and first threading hole and the second threading hole are mutually communicated.The circuit such as power line, control line winding magnet ring, is effectively ensured the normal work of horizontal stage electric machine when the utility model can prevent horizontal stage electric machine from rotating.
Description
Technical field
The utility model is related to aircraft head field, more particularly to a kind of horizontal stage electric machine, head and aircraft.
Background technology
Head plays connection and steering-effecting between optical device bottom and fixed support.In picture pick-up device, especially
There is provided in the aircraft of aerial photography function, head is generally driven using motor.The aircraft head of prior art it is main by motor and
Horn is constituted.Wherein, horizontal stage electric machine is mainly by stator, rotor and for detecting that the magnet ring of the axial angle of head horn is constituted.
Magnet ring is convexly equipped in the circuits such as the center of stator, control line, power line and is drawn from stator and internal rotor.
The horizontal stage electric machine used in the aircraft of prior art is in rotary course, and the circuit such as control line, power line is easy
Winding magnet ring, influences the normal work of motor.
Utility model content
Based on this, it is necessary to provide a kind of new horizontal stage electric machine, head and aircraft to avoid horizontal stage electric machine rotary course
Middle circuit winds magnet ring, and the normal work of horizontal stage electric machine is effectively ensured.
According to one side of the present utility model, the utility model provides a kind of horizontal stage electric machine, include rotor, stator and
Magnet ring, the first threading hole is provided with the centre position of the stator, the position of correspondence first threading hole on the rotor
The second threading hole is provided with, first threading hole and the second threading hole are mutually communicated.
Further, the magnet ring is fixed on the rotor by through the support column of first threading hole.
Further, it is additionally provided with support base on the rotor, the head is fixed on the end of the support column, and institute
The bottom for stating support column is then fixed on the support base.
Further, the support base located at second threading hole centre position, and with second threading hole
Hole edge connects.
Further, second threading hole is shaped as circle, and the support base is by second threading hole
Second threading hole is simultaneously separated at least two arcuate structures by the center of circle.
Further, institute's support base is shaped as linear structure, and being radially arranged along second threading hole.
Further, first threading hole is shaped as circle.
Further, the internal diameter of the internal diameter of second threading hole and first threading hole is all higher than the outer of the magnet ring
Footpath.
According to second aspect of the present utility model, the utility model provides a kind of head, and the head includes as above institute
The horizontal stage electric machine stated.
According to the 3rd aspect of the present utility model, the utility model provides a kind of aircraft, the aircraft include just like
Upper described head.
The beneficial effects of the utility model are：
Embodiment of the present utility model in the stator of motor and the center of rotor by setting connect the respectively
One threading hole and the second threading hole so that the circuit such as power line, control line can be penetrated/worn from the first threading hole and the second threading hole
Go out, so as to circuit winds magnet ring in avoiding motor rotary course, the normal work of motor has been effectively ensured.
Brief description of the drawings
In order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art, below will be to embodiment
Or the accompanying drawing to be used needed for description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is some embodiments of the present utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is one dimensional structure diagram of implementation method of horizontal stage electric machine of the present utility model.
Fig. 2 is one perspective exploded view of implementation method of horizontal stage electric machine of the present utility model.
Fig. 3 is one perspective exploded view of implementation method of horizontal stage electric machine of the present utility model.
Fig. 4 is the orthographic drawing of Fig. 3.
Fig. 5 is the A-A sectional views of Fig. 4.
Specific embodiment
Realization of the present utility model is described in detail below by specific embodiment combination accompanying drawing.
As Figure 1-Figure 5, one embodiment of the present utility model is mainly included：Stator 1, rotor 2 and magnet ring 3.It is fixed
Son 1 and rotor 2 convert electrical energy into the kinetic energy for driving cloud platform rotation or change in location in rotary course.Magnet ring 3 is used to detect
The axial angle of head horn, in three axle heads, motor on three head horns is total to be detected roll, goes off course, bows
The angle faced upward, i.e., roll, driftage, the luffing angle of camera on head.
The first threading hole 11 is provided with the centre position of the stator 1, correspondence first threading hole on the rotor 2
11 position is provided with the second threading hole 21, and the threading hole 12 of first threading hole 11 and second is mutually communicated so that power line, control
The circuits such as line processed can be penetrated from the first threading hole 11, passed from the second threading hole 12；Or penetrated from the second threading hole 12, first wears
String holes 11 is passed.
In an implementation method of the present utility model, the magnet ring 3 is by the support through first threading hole 11
Post 4 is fixed on the rotor 2.
It is additionally provided with support base 22 on the rotor 2, the head 3 is fixed on the end of the support column 4, and the branch
The bottom of dagger 4 is then fixed on the support base 22.
The support base 22 located at second threading hole 21 centre position, and with the hole edge of second threading hole 21
Connect.
Second threading hole 21 is shaped as circle, and the center of circle that the support base 22 passes through second threading hole 21
And second threading hole 21 is separated at least two arcuate structures.
In one embodiment of the present utility model, institute's support base 22 is shaped as linear structure, and along described second
Threading hole 21 is radially arranged.In this case, second threading hole 21 has been separated into two equities by institute's support base 22
Arcuate structure.It is understood that support base 22 can also be other structures, such as the folding in the center of circle of the second threading hole 21 as described in
Linear structure, so as to second threading hole 21 is separated into two not reciprocity arcuate structures；Or center and described second
" people " character form structure that the center of circle of threading hole 21 overlaps, so as to second threading hole 21 is separated into three arcuate structures etc..
It is not limited to the present embodiment.
In one embodiment of the present utility model, first threading hole 11 is shaped as circle.It is understood that
First threading hole 11 can also be other shapes.Correspondingly, second threading hole 21 can also be other shapes.
In order to reserve the indwelling space of the circuits such as power line, control line, the internal diameter of second threading hole 21 and described
The internal diameter of one threading hole 22 is all higher than the external diameter of the magnet ring 3.In one embodiment of the present utility model, first threading
The internal diameter of the threading hole 21 of hole 11 and second may be configured as identical.It is understood that can neatly pass/wear in guarantee circuit
On the premise of entering, first threading hole 11 is not necessarily identical with the internal diameter of the second threading hole 21, such as, and described first
The internal diameter of threading hole 11 can also be slightly larger than or be slightly less than the internal diameter of second threading hole 21.It is not limited to the present embodiment.
The invention also discloses a kind of head, motor and horn are included, in one embodiment, the motor is adopted
With the horizontal stage electric machine described in previous embodiment, repeat no more.
The invention also discloses a kind of aircraft, the aircraft is included just like the head described in previous embodiment,
Repeat no more.
Above content is to combine specific preferred embodiment further detailed description of the utility model, it is impossible to
Assert that specific implementation of the present utility model is confined to these explanations.For the ordinary skill of the utility model art
For personnel, without departing from the concept of the premise utility, some simple deduction or replace can also be made, should all regarded
To belong to protection domain of the present utility model.
Claims (10)
1. a kind of horizontal stage electric machine, includes rotor, stator and magnet ring, it is characterised in that be provided with the centre position of the stator
First threading hole, the position of correspondence first threading hole is provided with the second threading hole, first threading hole on the rotor
It is mutually communicated with the second threading hole.
2. horizontal stage electric machine as claimed in claim 1, it is characterised in that the magnet ring is by the branch through first threading hole
Dagger is fixed on the rotor.
3. horizontal stage electric machine as claimed in claim 2, it is characterised in that support base, the head are additionally provided with the rotor
The end of the support column is fixed on, and the bottom of the support column is then fixed on the support base.
4. horizontal stage electric machine as claimed in claim 3, it is characterised in that the support base is located at the centre of second threading hole
Position, and connect with the hole edge of second threading hole.
5. horizontal stage electric machine as claimed in claim 4, it is characterised in that second threading hole is shaped as circle, and described
Support base is separated at least two arcuate structures by the center of circle of second threading hole and by second threading hole.
6. horizontal stage electric machine as claimed in claim 5, it is characterised in that institute's support base is shaped as linear structure, and along institute
State being radially arranged for the second threading hole.
7. the horizontal stage electric machine as any one of claim 1-6, it is characterised in that first threading hole is shaped as circle
Shape.
8. the horizontal stage electric machine as any one of claim 1-6, it is characterised in that the internal diameter of second threading hole and institute
The internal diameter for stating the first threading hole is all higher than the external diameter of the magnet ring.
9. a kind of head, includes motor and horn, it is characterised in that the motor is such as any one of claim 1-8 institutes
The horizontal stage electric machine stated.
10. a kind of aircraft, it is characterised in that include head as claimed in claim 9.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621230631.3U CN206259837U (en) | 2016-11-16 | 2016-11-16 | Horizontal stage electric machine, head and aircraft |
| PCT/CN2017/107805 WO2018090808A1 (en) | 2016-11-16 | 2017-10-26 | Cradle head motor, cradle head and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621230631.3U CN206259837U (en) | 2016-11-16 | 2016-11-16 | Horizontal stage electric machine, head and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206259837U true CN206259837U (en) | 2017-06-16 |
Family
ID=59025916
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621230631.3U Active CN206259837U (en) | 2016-11-16 | 2016-11-16 | Horizontal stage electric machine, head and aircraft |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN206259837U (en) |
| WO (1) | WO2018090808A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018090808A1 (en) * | 2016-11-16 | 2018-05-24 | 亿航智能设备（广州）有限公司 | Cradle head motor, cradle head and aircraft |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204425121U (en) * | 2015-01-04 | 2015-06-24 | 广州虹天航空科技有限公司 | Motor module and tripod head equipment |
| CN105207408B (en) * | 2015-10-26 | 2018-01-30 | 深圳市道通智能航空技术有限公司 | A kind of motor, head and aircraft |
| CN105667818A (en) * | 2016-01-05 | 2016-06-15 | 零度智控（北京）智能科技有限公司 | Cradle head |
| CN106100221A (en) * | 2016-08-10 | 2016-11-09 | 深圳市固胜智能科技有限公司 | A kind of horizontal stage electric machine and The Cloud Terrace |
| CN206259837U (en) * | 2016-11-16 | 2017-06-16 | 广州亿航智能技术有限公司 | Horizontal stage electric machine, head and aircraft |
-
2016
- 2016-11-16 CN CN201621230631.3U patent/CN206259837U/en active Active
-
2017
- 2017-10-26 WO PCT/CN2017/107805 patent/WO2018090808A1/en active Application Filing
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018090808A1 (en) * | 2016-11-16 | 2018-05-24 | 亿航智能设备（广州）有限公司 | Cradle head motor, cradle head and aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2018090808A1 (en) | 2018-05-24 |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant |